Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe474-il-500000-n5 Airfoil,goe474-il Reynolds number,500000 Ncrit,5 Mach,0 Max Cl/Cd,85.0675 Max Cl/Cd alpha,2 Url,http://airfoiltools.com/polar/csv?polar=xf-goe474-il-500000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.750,-0.4649,0.09392,0.09158,-0.0253,1.0000,0.0064 -9.500,-0.4679,0.08945,0.08715,-0.0269,1.0000,0.0066 -9.000,-0.6767,0.02993,0.02678,-0.0593,0.9968,0.0057 -8.750,-0.6544,0.02519,0.02152,-0.0622,0.9927,0.0059 -8.500,-0.6274,0.02303,0.01909,-0.0639,0.9890,0.0061 -8.250,-0.5977,0.02145,0.01729,-0.0655,0.9864,0.0064 -8.000,-0.5707,0.02024,0.01589,-0.0662,0.9819,0.0068 -7.750,-0.5420,0.01878,0.01417,-0.0672,0.9785,0.0072 -7.500,-0.5130,0.01745,0.01257,-0.0680,0.9754,0.0077 -7.250,-0.4862,0.01626,0.01115,-0.0682,0.9704,0.0080 -7.000,-0.4569,0.01497,0.00960,-0.0690,0.9671,0.0085 -6.750,-0.4274,0.01405,0.00854,-0.0697,0.9633,0.0091 -6.500,-0.3989,0.01344,0.00783,-0.0700,0.9580,0.0098 -6.250,-0.3675,0.01288,0.00717,-0.0709,0.9541,0.0109 -6.000,-0.3372,0.01239,0.00657,-0.0715,0.9494,0.0118 -5.750,-0.3083,0.01169,0.00577,-0.0718,0.9436,0.0136 -5.500,-0.2768,0.01127,0.00529,-0.0726,0.9390,0.0155 -5.250,-0.2476,0.01092,0.00487,-0.0729,0.9326,0.0175 -5.000,-0.2177,0.01050,0.00438,-0.0733,0.9262,0.0202 -4.750,-0.1889,0.01019,0.00404,-0.0735,0.9195,0.0237 -4.500,-0.1601,0.00995,0.00370,-0.0737,0.9126,0.0267 -4.250,-0.1318,0.00976,0.00345,-0.0737,0.9057,0.0286 -4.000,-0.1045,0.00940,0.00302,-0.0735,0.8982,0.0326 -3.750,-0.0772,0.00916,0.00273,-0.0733,0.8908,0.0361 -3.500,-0.0499,0.00899,0.00247,-0.0731,0.8832,0.0387 -3.250,-0.0230,0.00877,0.00222,-0.0728,0.8760,0.0449 -3.000,0.0036,0.00851,0.00202,-0.0724,0.8687,0.0622 -2.750,0.0303,0.00835,0.00192,-0.0721,0.8617,0.0892 -2.500,0.0575,0.00827,0.00183,-0.0719,0.8545,0.1012 -2.250,0.0845,0.00819,0.00175,-0.0716,0.8471,0.1088 -2.000,0.1116,0.00815,0.00166,-0.0713,0.8399,0.1152 -1.750,0.1386,0.00808,0.00158,-0.0711,0.8329,0.1204 -1.500,0.1656,0.00803,0.00150,-0.0707,0.8247,0.1252 -1.250,0.1921,0.00799,0.00142,-0.0703,0.8135,0.1295 -1.000,0.2186,0.00795,0.00135,-0.0699,0.8015,0.1341 -0.750,0.2452,0.00791,0.00130,-0.0695,0.7909,0.1399 -0.500,0.2718,0.00789,0.00125,-0.0691,0.7806,0.1460 -0.250,0.2980,0.00785,0.00121,-0.0686,0.7671,0.1564 0.000,0.3240,0.00782,0.00118,-0.0681,0.7523,0.1686 0.250,0.3501,0.00780,0.00116,-0.0677,0.7382,0.1804 0.500,0.3758,0.00779,0.00114,-0.0671,0.7204,0.1945 0.750,0.4008,0.00780,0.00113,-0.0664,0.6961,0.2161 1.000,0.4255,0.00776,0.00114,-0.0657,0.6726,0.2593 1.250,0.4464,0.00718,0.00120,-0.0645,0.6528,0.5115 1.500,0.4944,0.00623,0.00137,-0.0687,0.6225,0.9765 1.750,0.5389,0.00642,0.00143,-0.0724,0.5889,0.9964 2.000,0.5674,0.00667,0.00149,-0.0727,0.5422,1.0000 2.250,0.5860,0.00713,0.00161,-0.0708,0.4644,1.0000 2.500,0.6055,0.00760,0.00180,-0.0691,0.4051,1.0000 2.750,0.6265,0.00798,0.00198,-0.0678,0.3600,1.0000 3.000,0.6482,0.00833,0.00216,-0.0666,0.3197,1.0000 3.250,0.6703,0.00865,0.00234,-0.0655,0.2856,1.0000 3.500,0.6924,0.00897,0.00252,-0.0644,0.2519,1.0000 3.750,0.7146,0.00931,0.00272,-0.0633,0.2203,1.0000 4.000,0.7370,0.00963,0.00293,-0.0622,0.1952,1.0000 4.250,0.7598,0.00992,0.00316,-0.0613,0.1762,1.0000 4.500,0.7825,0.01023,0.00340,-0.0603,0.1588,1.0000 4.750,0.8056,0.01052,0.00364,-0.0594,0.1447,1.0000 5.000,0.8288,0.01080,0.00389,-0.0585,0.1309,1.0000 5.250,0.8521,0.01108,0.00414,-0.0577,0.1196,1.0000 5.500,0.8754,0.01137,0.00441,-0.0568,0.1089,1.0000 5.750,0.8981,0.01171,0.00470,-0.0559,0.0963,1.0000 6.000,0.9209,0.01206,0.00500,-0.0550,0.0856,1.0000 6.250,0.9438,0.01239,0.00534,-0.0541,0.0765,1.0000 6.500,0.9669,0.01270,0.00566,-0.0533,0.0678,1.0000 6.750,0.9891,0.01311,0.00601,-0.0523,0.0534,1.0000 7.000,1.0093,0.01372,0.00649,-0.0511,0.0342,1.0000 7.250,1.0293,0.01437,0.00706,-0.0499,0.0210,1.0000 7.500,1.0502,0.01493,0.00764,-0.0487,0.0156,1.0000 7.750,1.0714,0.01546,0.00822,-0.0476,0.0127,1.0000 8.000,1.0925,0.01599,0.00882,-0.0464,0.0110,1.0000 8.250,1.1126,0.01662,0.00949,-0.0452,0.0097,1.0000 8.500,1.1319,0.01735,0.01030,-0.0438,0.0087,1.0000 8.750,1.1520,0.01795,0.01100,-0.0426,0.0082,1.0000 9.000,1.1712,0.01863,0.01177,-0.0413,0.0076,1.0000 9.250,1.1897,0.01934,0.01257,-0.0399,0.0071,1.0000 9.500,1.2076,0.02009,0.01341,-0.0384,0.0066,1.0000 9.750,1.2222,0.02114,0.01455,-0.0365,0.0062,1.0000 10.000,1.2383,0.02197,0.01548,-0.0349,0.0058,1.0000 10.250,1.2539,0.02279,0.01642,-0.0331,0.0055,1.0000 10.500,1.2664,0.02380,0.01755,-0.0309,0.0053,1.0000 10.750,1.2773,0.02475,0.01861,-0.0285,0.0051,1.0000 11.000,1.2861,0.02581,0.01979,-0.0258,0.0049,1.0000 11.250,1.2950,0.02685,0.02094,-0.0233,0.0047,1.0000 11.500,1.3021,0.02804,0.02225,-0.0207,0.0046,1.0000 11.750,1.3083,0.02929,0.02362,-0.0183,0.0045,1.0000 12.000,1.3138,0.03060,0.02503,-0.0160,0.0043,1.0000 12.250,1.3153,0.03231,0.02687,-0.0135,0.0043,1.0000 12.500,1.3124,0.03445,0.02919,-0.0110,0.0041,1.0000 12.750,1.3079,0.03687,0.03177,-0.0089,0.0040,1.0000 13.000,1.3035,0.03944,0.03450,-0.0071,0.0040,1.0000 13.250,1.3034,0.04171,0.03695,-0.0060,0.0039,1.0000 13.500,1.2976,0.04474,0.04016,-0.0051,0.0039,1.0000 13.750,1.2908,0.04811,0.04372,-0.0047,0.0038,1.0000 14.000,1.2810,0.05209,0.04789,-0.0050,0.0038,1.0000 14.250,1.2705,0.05648,0.05246,-0.0059,0.0038,1.0000 14.500,1.2585,0.06150,0.05765,-0.0076,0.0037,1.0000 14.750,1.2428,0.06754,0.06387,-0.0102,0.0038,1.0000 15.000,1.2269,0.07432,0.07082,-0.0138,0.0038,1.0000 15.250,1.2104,0.08199,0.07866,-0.0183,0.0038,1.0000 15.500,1.1904,0.09092,0.08777,-0.0236,0.0037,1.0000 15.750,1.1689,0.10027,0.09726,-0.0290,0.0038,1.0000 16.000,1.1477,0.10989,0.10701,-0.0344,0.0038,1.0000